Coordinate measurement machines with removable accessories

ABSTRACT

A portable articulated arm coordinate measuring machine is provided. The coordinate measuring machine includes a base with an arm portion. A probe end is coupled to an end of the arm portion distal from the base. A device configured to emit a coded structured light onto an object to determine the three dimensional coordinates of a point on the object.

CROSS-REFERENCE TO RELATED APPLICATIONS

The present application is a continuation-in-part of U.S. patentapplication Ser. No. 13/006,507 filed Jan. 14, 2011, and claims thebenefit of provisional application No. 61/296,555 filed Jan. 20, 2010,provisional application No. 61/355,279 filed Jun. 16, 2010, andprovisional application No. 61/351,347 filed on Jun. 4, 2010, thecontents of which are hereby incorporated by reference in theirentirety.

BACKGROUND

The present disclosure relates to a coordinate measuring machine, andmore particularly to a portable articulated arm coordinate measuringmachine having a connector on a probe end of the coordinate measuringmachine that allows accessory devices which use structured light fornon-contact three dimensional measurement to be removably connected tothe coordinate measuring machine.

Portable articulated arm coordinate measuring machines (AACMMs) havefound widespread use in the manufacturing or production of parts wherethere is a need to rapidly and accurately verify the dimensions of thepart during various stages of the manufacturing or production (e.g.,machining) of the part. Portable AACMMs represent a vast improvementover known stationary or fixed, cost-intensive and relatively difficultto use measurement installations, particularly in the amount of time ittakes to perform dimensional measurements of relatively complex parts.Typically, a user of a portable AACMM simply guides a probe along thesurface of the part or object to be measured. The measurement data arethen recorded and provided to the user. In some cases, the data areprovided to the user in visual form, for example, three-dimensional(3-D) form on a computer screen. In other cases, the data are providedto the user in numeric form, for example when measuring the diameter ofa hole, the text “Diameter=1.0034” is displayed on a computer screen.

An example of a prior art portable articulated arm CMM is disclosed incommonly assigned U.S. Pat. No. 5,402,582 ('582), which is incorporatedherein by reference in its entirety. The '582 patent discloses a 3-Dmeasuring system comprised of a manually-operated articulated arm CMMhaving a support base on one end and a measurement probe at the otherend. Commonly assigned U.S. Pat. No. 5,611,147 ('147), which isincorporated herein by reference in its entirety, discloses a similararticulated arm CMM. In the '147 patent, the articulated arm CMMincludes a number of features including an additional rotational axis atthe probe end, thereby providing for an arm with either a two-two-two ora two-two-three axis configuration (the latter case being a seven axisarm).

Three-dimensional surfaces may be measured using non-contact techniquesas well. One type of non-contact device, sometimes referred to as alaser line probe or laser line scanner, emits a laser light either on aspot, or along a line. An imaging device, such as a charge-coupleddevice (CCD) for example, is positioned adjacent the laser. The laser isarranged to emit a line of light which is reflected off of the surface.The surface of the object being measured causes a diffuse reflectionwhich is captured by the imaging device. The image of the reflected lineon the sensor will change as the distance between the sensor and thesurface changes. By knowing the relationship between the imaging sensorand the laser and the position of the laser image on the sensor,triangulation methods may be used to measure three-dimensionalcoordinates of points on the surface. One issue that arises with laserline probes, is that the density of measured points may vary dependingon the speed at which the laser line probe is moved across the surfaceof the object. The faster the laser line probe is moved, the greater thedistance between the points and a lower point density. With a structuredlight scanner, the point spacing is typically uniform in each of the twodimensions, thereby generally providing uniform measurement of workpiecesurface points.

While existing CMM's are suitable for their intended purposes, what isneeded is a portable AACMM that has certain features of embodiments ofthe present invention.

SUMMARY OF THE INVENTION

In accordance with one embodiment of the invention, a portablearticulated arm coordinate measuring machine (AACMM) for measuringthree-dimensional coordinates of an object in space is provided. TheAACMM includes a base. A manually positionable arm portion is providedhaving an opposed first end and second end, the arm portion beingrotationally coupled to the base, the arm portion including a pluralityof connected arm segments, each arm segment including at least oneposition transducer for producing a position signal. An electroniccircuit is provided that receives the position signal from the at leastone position transducer in each arm segment. A probe end is coupled tothe first end. A noncontact three-dimensional measuring device iscoupled to the probe end, the noncontact three-dimensional measuringdevice having a projector and an image sensor, the projector having asource plane, the projector configured to emit a structured light ontothe object, the structured light located on the source plane andincluding at least three non-collinear pattern elements, the imagesensor arranged to receive the structured light reflected from theobject. A processor is electrically coupled to the electronic circuit,the processor configured to determine the three-dimensional coordinatesof a point on the object in response to receiving the position signalsfrom the position transducers and in response to receiving thestructured light by the image sensor.

In accordance with one embodiment of the invention, a method ofoperating a portable articulated arm coordinate measuring machine formeasuring the coordinates of an object in space is provided. The methodincludes providing a manually positionable arm portion having an opposedfirst end and second end, the arm portion including a plurality ofconnected arm segments, each arm segment including at least one positiontransducer for producing a position signal. A probe end is provided formeasuring the object, the probe end being coupled to the first end. Anelectronic circuit receives the position signals from the transducers. Athree-dimensional noncontact measurement device is provided having acontroller, the three-dimensional noncontact measurement device having asensor and a projector, the projector configured to emit a structuredlight onto the object, the projector having a source plane, thestructured light located on the source plane and including at leastthree non-collinear pattern elements. A structured light is projectedfrom the three-dimensional measurement device onto the object.

BRIEF DESCRIPTION OF THE DRAWINGS

Referring now to the drawings, exemplary embodiments are shown whichshould not be construed to be limiting regarding the entire scope of thedisclosure, and wherein the elements are numbered alike in severalFIGURES:

FIG. 1, including FIGS. 1A and 1B, are perspective views of a portablearticulated arm coordinate measuring machine (AACMM) having embodimentsof various aspects of the present invention therewithin;

FIG. 2, including FIGS. 2A-2D taken together, is a block diagram ofelectronics utilized as part of the AACMM of FIG. 1 in accordance withan embodiment;

FIG. 3, including FIGS. 3A and 3B taken together, is a block diagramdescribing detailed features of the electronic data processing system ofFIG. 2 in accordance with an embodiment;

FIG. 4 is an isometric view of the probe end of the AACMM of FIG. 1;

FIG. 5 is a side view of the probe end of FIG. 4 with the handle beingcoupled thereto;

FIG. 6 is a side view of the probe end of FIG. 4 with the handleattached;

FIG. 7 is an enlarged partial side view of the interface portion of theprobe end of FIG. 6;

FIG. 8 is another enlarged partial side view of the interface portion ofthe probe end of FIG. 5;

FIG. 9 is an isometric view partially in section of the handle of FIG.4;

FIG. 10 is an isometric view of the probe end of the AACMM of FIG. 1with a structured light device having a single camera attached;

FIG. 11 is an isometric view partially in section of the device of FIG.10;

FIG. 12 is an isometric view of the probe end of the AACMM of FIG. 1with another structured light device having dual cameras attached;

FIG. 13A and FIG. 13B are schematic views illustrating the operation ofthe device of FIG. 10 when attached to the probe end of the AACMM ofFIG. 1;

FIGS. 14-17 are sequential projections having an uncoded binary patternthat may be emitted by the structured light device of FIG. 10 or FIG.12, in accordance with an embodiment of the present invention;

FIGS. 18-19 are spatially varying color coded patterns that may beemitted by the structured light device of FIG. 10 or FIG. 12, inaccordance with an embodiment of the invention;

FIGS. 20-23 are strip index coded patterns that may be emitted by thestructured light device of FIG. 10 or FIG. 12, in accordance with anembodiment of the invention;

FIGS. 24-31 are two-dimensional grid patterns that may be emitted by thestructured light device of FIG. 10 or FIG. 12, in accordance with anembodiment of the invention;

FIG. 32 is a schematic illustration of a photometric technique foracquiring patterns of structured light under a plurality of lightingconditions; and,

FIG. 33 is an illustration of a structured light scanner deviceindependently operable from an AACMM in accordance with anotherembodiment of the invention.

DETAILED DESCRIPTION

Portable articulated arm coordinate measuring machines (“AACMM”) areused in a variety of applications to obtain measurements of objects.Embodiments of the present invention provide advantages in allowing anoperator to easily and quickly couple accessory devices to a probe endof the AACMM that use structured light to provide for the non-contactmeasuring of a three-dimensional object. Embodiments of the presentinvention provide further advantages in providing for communicating datarepresenting a point cloud measured by the structured light devicewithin the AACMM. Embodiments of the present invention provideadvantages in greater uniformity in the distribution of measured pointsthat may provide enhanced accuracy. Embodiments of the present inventionprovide still further advantages in providing power and datacommunications to a removable accessory without having externalconnections or wiring.

As used herein, the term “structured light” refers to a two-dimensionalpattern of light projected onto a continuous and enclosed area of anobject that conveys information which may be used to determinecoordinates of points on the object. A structured light pattern willcontain at least three non-collinear pattern elements disposed withinthe contiguous and enclosed area. Each of the three non-collinearpattern elements conveys information which may be used to determine thepoint coordinates.

In general, there are two types of structured light, a coded lightpattern and an uncoded light pattern. As used herein a coded lightpattern is one in which the three dimensional coordinates of anilluminated surface of the object may be ascertained by the acquisitionof a single image. In some cases, the projecting device may be movingrelative to the object. In other words, for a coded light pattern therewill be no significant temporal relationship between the projectedpattern and the acquired image. Typically, a coded light pattern willcontain a set of elements (e.g. geometric shapes) arranged so that atleast three of the elements are non-collinear. In some cases, the set ofelements may be arranged into collections of lines. Having at leastthree of the element be non-collinear ensures that the pattern is not asimple line pattern as would be projected, for example, by a laser linescanner. As a result, the pattern elements are recognizable because ofthe arrangement of the elements.

In contrast, an uncoded structured light pattern as used herein is apattern that does not allow measurement through a single pattern whenthe projector is moving relative to the object. An example of an uncodedlight pattern is one which requires a series of sequential patterns andthus the acquisition of a series of sequential images. Due to thetemporal nature of the projection pattern and acquisition of the image,there should be no relative movement between the projector and theobject.

It should be appreciated that structured light is different from lightprojected by a laser line probe or laser line scanner type device thatgenerates a line of light. To the extent that laser line probes usedwith articulated arms today have irregularities or other aspects thatmay be regarded as features within the generated lines, these featuresare disposed in a collinear arrangement. Consequently such featureswithin a single generated line are not considered to make the projectedlight into structured light.

FIGS. 1A and 1B illustrate, in perspective, an AACMM 100 according tovarious embodiments of the present invention, an articulated arm beingone type of coordinate measuring machine. As shown in FIGS. 1A and 1B,the exemplary AACMM 100 may comprise a six or seven axis articulatedmeasurement device having a probe end 401 that includes a measurementprobe housing 102 coupled to an arm portion 104 of the AACMM 100 at oneend. The arm portion 104 comprises a first arm segment 106 coupled to asecond arm segment 108 by a first grouping of bearing cartridges 110(e.g., two bearing cartridges). A second grouping of bearing cartridges112 (e.g., two bearing cartridges) couples the second arm segment 108 tothe measurement probe housing 102. A third grouping of bearingcartridges 114 (e.g., three bearing cartridges) couples the first armsegment 106 to a base 116 located at the other end of the arm portion104 of the AACMM 100. Each grouping of bearing cartridges 110, 112, 114provides for multiple axes of articulated movement. Also, the probe end401 may include a measurement probe housing 102 that comprises the shaftof the seventh axis portion of the AACMM 100 (e.g., a cartridgecontaining an encoder system that determines movement of the measurementdevice, for example a probe 118, in the seventh axis of the AACMM 100).In this embodiment, the probe end 401 may rotate about an axis extendingthrough the center of measurement probe housing 102. In use of the AACMM100, the base 116 is typically affixed to a work surface.

Each bearing cartridge within each bearing cartridge grouping 110, 112,114 typically contains an encoder system (e.g., an optical angularencoder system). The encoder system (i.e., transducer) provides anindication of the position of the respective arm segments 106, 108 andcorresponding bearing cartridge groupings 110, 112, 114 that alltogether provide an indication of the position of the probe 118 withrespect to the base 116 (and, thus, the position of the object beingmeasured by the AACMM 100 in a certain frame of reference—for example alocal or global frame of reference). The arm segments 106, 108 may bemade from a suitably rigid material such as but not limited to a carboncomposite material for example. A portable AACMM 100 with six or sevenaxes of articulated movement (i.e., degrees of freedom) providesadvantages in allowing the operator to position the probe 118 in adesired location within a 360° area about the base 116 while providingan arm portion 104 that may be easily handled by the operator. However,it should be appreciated that the illustration of an arm portion 104having two arm segments 106, 108 is for exemplary purposes, and theclaimed invention should not be so limited. An AACMM 100 may have anynumber of arm segments coupled together by bearing cartridges (and,thus, more or less than six or seven axes of articulated movement ordegrees of freedom).

The probe 118 is detachably mounted to the measurement probe housing102, which is connected to bearing cartridge grouping 112. A handle 126is removable with respect to the measurement probe housing 102 by wayof, for example, a quick-connect interface. As will be discussed in moredetail below, the handle 126 may be replaced with another deviceconfigured to emit a structured light to provide non-contact measurementof three-dimensional objects, thereby providing advantages in allowingthe operator to make both contact and non-contact measurements with thesame AACMM 100. In exemplary embodiments, the probe housing 102 houses aremovable probe 118, which is a contacting measurement device and mayhave different tips 118 that physically contact the object to bemeasured, including, but not limited to: ball, touch-sensitive, curvedand extension type probes. In other embodiments, the measurement isperformed, for example, by a non-contacting device such as a codedstructured light scanner device. In an embodiment, the handle 126 isreplaced with the coded structured light scanner device using thequick-connect interface. Other types of measurement devices may replacethe removable handle 126 to provide additional functionality. Examplesof such measurement devices include, but are not limited to, one or moreillumination lights, a temperature sensor, a thermal scanner, a bar codescanner, a projector, a paint sprayer, a camera, or the like, forexample.

As shown in FIGS. 1A and 1B, the AACMM 100 includes the removable handle126 that provides advantages in allowing accessories or functionality tobe changed without removing the measurement probe housing 102 from thebearing cartridge grouping 112. As discussed in more detail below withrespect to FIG. 2D, the removable handle 126 may also include anelectrical connector that allows electrical power and data to beexchanged with the handle 126 and the corresponding electronics locatedin the probe end 401.

In various embodiments, each grouping of bearing cartridges 110, 112,114 allows the arm portion 104 of the AACMM 100 to move about multipleaxes of rotation. As mentioned, each bearing cartridge grouping 110,112, 114 includes corresponding encoder systems, such as optical angularencoders for example, that are each arranged coaxially with thecorresponding axis of rotation of, e.g., the arm segments 106, 108. Theoptical encoder system detects rotational (swivel) or transverse (hinge)movement of, e.g., each one of the arm segments 106, 108 about thecorresponding axis and transmits a signal to an electronic dataprocessing system within the AACMM 100 as described in more detailherein below. Each individual raw encoder count is sent separately tothe electronic data processing system as a signal where it is furtherprocessed into measurement data. No position calculator separate fromthe AACMM 100 itself (e.g., a serial box) is required, as disclosed incommonly assigned U.S. Pat. No. 5,402,582 ('582).

The base 116 may include an attachment device or mounting device 120.The mounting device 120 allows the AACMM 100 to be removably mounted toa desired location, such as an inspection table, a machining center, awall or the floor for example. In one embodiment, the base 116 includesa handle portion 122 that provides a convenient location for theoperator to hold the base 116 as the AACMM 100 is being moved. In oneembodiment, the base 116 further includes a movable cover portion 124that folds down to reveal a user interface, such as a display screen.

In accordance with an embodiment, the base 116 of the portable AACMM 100contains or houses an electronic circuit having an electronic dataprocessing system that includes two primary components: a baseprocessing system that processes the data from the various encodersystems within the AACMM 100 as well as data representing other armparameters to support three-dimensional (3-D) positional calculations;and a user interface processing system that includes an on-boardoperating system, a touch screen display, and resident applicationsoftware that allows for relatively complete metrology functions to beimplemented within the AACMM 100 without the need for connection to anexternal computer.

The electronic data processing system in the base 116 may communicatewith the encoder systems, sensors, and other peripheral hardware locatedaway from the base 116 (e.g., a structured light device that can bemounted to the removable handle 126 on the AACMM 100). The electronicsthat support these peripheral hardware devices or features may belocated in each of the bearing cartridge groupings 110, 112, 114 locatedwithin the portable AACMM 100.

FIG. 2 is a block diagram of electronics utilized in an AACMM 100 inaccordance with an embodiment. The embodiment shown in FIG. 2A includesan electronic data processing system 210 including a base processorboard 204 for implementing the base processing system, a user interfaceboard 202, a base power board 206 for providing power, a Bluetoothmodule 232, and a base tilt board 208. The user interface board 202includes a computer processor for executing application software toperform user interface, display, and other functions described herein.

As shown in FIG. 2A and FIG. 2B, the electronic data processing system210 is in communication with the aforementioned plurality of encodersystems via one or more arm buses 218. In the embodiment depicted inFIG. 2B and FIG. 2C, each encoder system generates encoder data andincludes: an encoder arm bus interface 214, an encoder digital signalprocessor (DSP) 216, an encoder read head interface 234, and atemperature sensor 212. Other devices, such as strain sensors, may beattached to the arm bus 218.

Also shown in FIG. 2D are probe end electronics 230 that are incommunication with the arm bus 218. The probe end electronics 230include a probe end DSP 228, a temperature sensor 212, a handle/deviceinterface bus 240 that connects with the handle 126 or the codedstructured light scanner device 242 via the quick-connect interface inan embodiment, and a probe interface 226. The quick-connect interfaceallows access by the handle 126 to the data bus, control lines, andpower bus used by the coded structured light scanner device 242 andother accessories. In an embodiment, the probe end electronics 230 arelocated in the measurement probe housing 102 on the AACMM 100. In anembodiment, the handle 126 may be removed from the quick-connectinterface and measurement may be performed by the structured lightdevice 242 communicating with the probe end electronics 230 of the AACMM100 via the interface bus 240. In an embodiment, the electronic dataprocessing system 210 is located in the base 116 of the AACMM 100, theprobe end electronics 230 are located in the measurement probe housing102 of the AACMM 100, and the encoder systems are located in the bearingcartridge groupings 110, 112, 114. The probe interface 226 may connectwith the probe end DSP 228 by any suitable communications protocol,including commercially-available products from Maxim IntegratedProducts, Inc. that embody the 1-wire® communications protocol 236.

FIG. 3 is a block diagram describing detailed features of the electronicdata processing system 210 of the AACMM 100 in accordance with anembodiment. In an embodiment, the electronic data processing system 210is located in the base 116 of the AACMM 100 and includes the baseprocessor board 204, the user interface board 202, a base power board206, a Bluetooth module 232, and a base tilt module 208.

In an embodiment shown in FIG. 3A, the base processor board 204 includesthe various functional blocks illustrated therein. For example, a baseprocessor function 302 is utilized to support the collection ofmeasurement data from the AACMM 100 and receives raw arm data (e.g.,encoder system data) via the arm bus 218 and a bus control modulefunction 308. The memory function 304 stores programs and static armconfiguration data. The base processor board 204 also includes anexternal hardware option port function 310 for communicating with anyexternal hardware devices or accessories such as a coded structuredlight scanner device 242. A real time clock (RTC) and log 306, a batterypack interface (IF) 316, and a diagnostic port 318 are also included inthe functionality in an embodiment of the base processor board 204depicted in FIG. 3A.

The base processor board 204 also manages all the wired and wirelessdata communication with external (host computer) and internal (displayprocessor 202) devices. The base processor board 204 has the capabilityof communicating with an Ethernet network via an Ethernet function 320(e.g., using a clock synchronization standard such as Institute ofElectrical and Electronics Engineers (IEEE) 1588), with a wireless localarea network (WLAN) via a LAN function 322, and with Bluetooth module232 via a parallel to serial communications (PSC) function 314. The baseprocessor board 204 also includes a connection to a universal serial bus(USB) device 312.

The base processor board 204 transmits and collects raw measurement data(e.g., encoder system counts, temperature readings) for processing intomeasurement data without the need for any preprocessing, such asdisclosed in the serial box of the aforementioned '582 patent. The baseprocessor 204 sends the processed data to the display processor 328 onthe user interface board 202 via an RS485 interface (IF) 326. In anembodiment, the base processor 204 also sends the raw measurement datato an external computer.

Turning now to the user interface board 202 in FIG. 3B, the angle andpositional data received by the base processor is utilized byapplications executing on the display processor 328 to provide anautonomous metrology system within the AACMM 100. Applications may beexecuted on the display processor 328 to support functions such as, butnot limited to: measurement of features, guidance and training graphics,remote diagnostics, temperature corrections, control of variousoperational features, connection to various networks, and display ofmeasured objects. Along with the display processor 328 and a liquidcrystal display (LCD) 338 (e.g., a touch screen LCD) user interface, theuser interface board 202 includes several interface options including asecure digital (SD) card interface 330, a memory 332, a USB Hostinterface 334, a diagnostic port 336, a camera port 340, an audio/videointerface 342, a dial-up/cell modem 344 and a global positioning system(GPS) port 346.

The electronic data processing system 210 shown in FIG. 3A also includesa base power board 206 with an environmental recorder 362 for recordingenvironmental data. The base power board 206 also provides power to theelectronic data processing system 210 using an AC/DC converter 358 and abattery charger control 360. The base power board 206 communicates withthe base processor board 204 using inter-integrated circuit (I2C) serialsingle ended bus 354 as well as via a DMA serial peripheral interface(DSPI) 357. The base power board 206 is connected to a tilt sensor andradio frequency identification (RFID) module 208 via an input/output(I/O) expansion function 364 implemented in the base power board 206.

Though shown as separate components, in other embodiments all or asubset of the components may be physically located in differentlocations and/or functions combined in different manners than that shownin FIG. 3A and FIG. 3B. For example, in one embodiment, the baseprocessor board 204 and the user interface board 202 are combined intoone physical board.

Referring now to FIGS. 4-9, an exemplary embodiment of a probe end 401is illustrated having a measurement probe housing 102 with aquick-connect mechanical and electrical interface that allows removableand interchangeable device 400 to couple with AACMM 100. In theexemplary embodiment, the device 400 includes an enclosure 402 thatincludes a handle portion 404 that is sized and shaped to be held in anoperator's hand, such as in a pistol grip for example. The enclosure 402is a thin wall structure having a cavity 406 (FIG. 9). The cavity 406 issized and configured to receive a controller 408. The controller 408 maybe a digital circuit, having a microprocessor for example, or an analogcircuit. In one embodiment, the controller 408 is in asynchronousbidirectional communication with the electronic data processing system210 (FIGS. 2 and 3). The communication connection between the controller408 and the electronic data processing system 210 may be wired (e.g. viacontroller 420) or may be a direct or indirect wireless connection (e.g.Bluetooth or IEEE 802.11) or a combination of wired and wirelessconnections. In the exemplary embodiment, the enclosure 402 is formed intwo halves 410, 412, such as from an injection molded plastic materialfor example. The halves 410, 412 may be secured together by fasteners,such as screws 414 for example. In other embodiments, the enclosurehalves 410, 412 may be secured together by adhesives or ultrasonicwelding for example.

The handle portion 404 also includes buttons or actuators 416, 418 thatmay be manually activated by the operator. The actuators 416, 418 arecoupled to the controller 408 that transmits a signal to a controller420 within the probe housing 102. In the exemplary embodiments, theactuators 416, 418 perform the functions of actuators 422, 424 locatedon the probe housing 102 opposite the device 400. It should beappreciated that the device 400 may have additional switches, buttons orother actuators that may also be used to control the device 400, theAACMM 100 or vice versa. Also, the device 400 may include indicators,such as light emitting diodes (LEDs), sound generators, meters, displaysor gauges for example. In one embodiment, the device 400 may include adigital voice recorder that allows for synchronization of verbalcomments with a measured point. In yet another embodiment, the device400 includes a microphone that allows the operator to transmit voiceactivated commands to the electronic data processing system 210.

In one embodiment, the handle portion 404 may be configured to be usedwith either operator hand or for a particular hand (e.g. left handed orright handed). The handle portion 404 may also be configured tofacilitate operators with disabilities (e.g. operators with missingfinders or operators with prosthetic arms). Further, the handle portion404 may be removed and the probe housing 102 used by itself whenclearance space is limited. As discussed above, the probe end 401 mayalso comprise the shaft of the seventh axis of AACMM 100. In thisembodiment the device 400 may be arranged to rotate about the AACMMseventh axis.

The probe end 401 includes a mechanical and electrical interface 426having a first connector 429 (FIG. 8) on the device 400 that cooperateswith a second connector 428 on the probe housing 102. The connectors428, 429 may include electrical and mechanical features that allow forcoupling of the device 400 to the probe housing 102. In one embodiment,the interface 426 includes a first surface 430 having a mechanicalcoupler 432 and an electrical connector 434 thereon. The enclosure 402also includes a second surface 436 positioned adjacent to and offsetfrom the first surface 430. In the exemplary embodiment, the secondsurface 436 is a planar surface offset a distance of approximately 0.5inches from the first surface 430. This offset provides a clearance forthe operator's fingers when tightening or loosening a fastener such ascollar 438. The interface 426 provides for a relatively quick and secureelectronic connection between the device 400 and the probe housing 102without the need to align connector pins, and without the need forseparate cables or connectors.

The electrical connector 434 extends from the first surface 430 andincludes one or more connector pins 440 that are electrically coupled inasynchronous bidirectional communication with the electronic dataprocessing system 210 (FIGS. 2 and 3), such as via one or more arm buses218 for example. The bidirectional communication connection may be wired(e.g. via arm bus 218), wireless (e.g. Bluetooth or IEEE 802.11), or acombination of wired and wireless connections. In one embodiment, theelectrical connector 434 is electrically coupled to the controller 420.The controller 420 may be in asynchronous bidirectional communicationwith the electronic data processing system 210 such as via one or morearm buses 218 for example. The electrical connector 434 is positioned toprovide a relatively quick and secure electronic connection withelectrical connector 442 on probe housing 102. The electrical connectors434, 442 connect with each other when the device 400 is attached to theprobe housing 102. The electrical connectors 434, 442 may each comprisea metal encased connector housing that provides shielding fromelectromagnetic interference as well as protecting the connector pinsand assisting with pin alignment during the process of attaching thedevice 400 to the probe housing 102.

The mechanical coupler 432 provides relatively rigid mechanical couplingbetween the device 400 and the probe housing 102 to support relativelyprecise applications in which the location of the device 400 on the endof the arm portion 104 of the AACMM 100 preferably does not shift ormove. Any such movement may typically cause an undesirable degradationin the accuracy of the measurement result. These desired results areachieved using various structural features of the mechanical attachmentconfiguration portion of the quick connect mechanical and electronicinterface of an embodiment of the present invention.

In one embodiment, the mechanical coupler 432 includes a firstprojection 444 positioned on one end 448 (the leading edge or “front” ofthe device 400). The first projection 444 may include a keyed, notchedor ramped interface that forms a lip 446 that extends from the firstprojection 444. The lip 446 is sized to be received in a slot 450defined by a projection 452 extending from the probe housing 102 (FIG.8). It should be appreciated that the first projection 444 and the slot450 along with the collar 438 form a coupler arrangement such that whenthe lip 446 is positioned within the slot 450, the slot 450 may be usedto restrict both the longitudinal and lateral movement of the device 400when attached to the probe housing 102. As will be discussed in moredetail below, the rotation of the collar 438 may be used to secure thelip 446 within the slot 450.

Opposite the first projection 444, the mechanical coupler 432 mayinclude a second projection 454. The second projection 454 may have akeyed, notched-lip or ramped interface surface 456 (FIG. 5). The secondprojection 454 is positioned to engage a fastener associated with theprobe housing 102, such as collar 438 for example. As will be discussedin more detail below, the mechanical coupler 432 includes a raisedsurface projecting from surface 430 that adjacent to or disposed aboutthe electrical connector 434 which provides a pivot point for theinterface 426 (FIGS. 7 and 8). This serves as the third of three pointsof mechanical contact between the device 400 and the probe housing 102when the device 400 is attached thereto.

The probe housing 102 includes a collar 438 arranged co-axially on oneend. The collar 438 includes a threaded portion that is movable betweena first position (FIG. 5) and a second position (FIG. 7). By rotatingthe collar 438, the collar 438 may be used to secure or remove thedevice 400 without the need for external tools. Rotation of the collar438 moves the collar 438 along a relatively coarse, square-threadedcylinder 474. The use of such relatively large size, square-thread andcontoured surfaces allows for significant clamping force with minimalrotational torque. The coarse pitch of the threads of the cylinder 474further allows the collar 438 to be tightened or loosened with minimalrotation.

To couple the device 400 to the probe housing 102, the lip 446 isinserted into the slot 450 and the device is pivoted to rotate thesecond projection 454 toward surface 458 as indicated by arrow 464 (FIG.5). The collar 438 is rotated causing the collar 438 to move ortranslate in the direction indicated by arrow 462 into engagement withsurface 456. The movement of the collar 438 against the angled surface456 drives the mechanical coupler 432 against the raised surface 460.This assists in overcoming potential issues with distortion of theinterface or foreign objects on the surface of the interface that couldinterfere with the rigid seating of the device 400 to the probe housing102. The application of force by the collar 438 on the second projection454 causes the mechanical coupler 432 to move forward pressing the lip446 into a seat on the probe housing 102. As the collar 438 continues tobe tightened, the second projection 454 is pressed upward toward theprobe housing 102 applying pressure on a pivot point. This provides asee-saw type arrangement, applying pressure to the second projection454, the lip 446 and the center pivot point to reduce or eliminateshifting or rocking of the device 400. The pivot point presses directlyagainst the bottom on the probe housing 102 while the lip 446 is appliesa downward force on the end of probe housing 102. FIG. 5 includes arrows462, 464 to show the direction of movement of the device 400 and thecollar 438. FIG. 7 includes arrows 466, 468, 470 to show the directionof applied pressure within the interface 426 when the collar 438 istightened. It should be appreciated that the offset distance of thesurface 436 of device 400 provides a gap 472 between the collar 438 andthe surface 436 (FIG. 6). The gap 472 allows the operator to obtain afirmer grip on the collar 438 while reducing the risk of pinchingfingers as the collar 438 is rotated. In one embodiment, the probehousing 102 is of sufficient stiffness to reduce or prevent thedistortion when the collar 438 is tightened.

Embodiments of the interface 426 allow for the proper alignment of themechanical coupler 432 and electrical connector 434 and also protectsthe electronics interface from applied stresses that may otherwise arisedue to the clamping action of the collar 438, the lip 446 and thesurface 456. This provides advantages in reducing or eliminating stressdamage to circuit board 476 mounted electrical connectors 434, 442 thatmay have soldered terminals. Also, embodiments provide advantages overknown approaches in that no tools are required for a user to connect ordisconnect the device 400 from the probe housing 102. This allows theoperator to manually connect and disconnect the device 400 from theprobe housing 102 with relative ease.

Due to the relatively large number of shielded electrical connectionspossible with the interface 426, a relatively large number of functionsmay be shared between the AACMM 100 and the device 400. For example,switches, buttons or other actuators located on the AACMM 100 may beused to control the device 400 or vice versa. Further, commands and datamay be transmitted from electronic data processing system 210 to thedevice 400. In one embodiment, the device 400 is a video camera thattransmits data of a recorded image to be stored in memory on the baseprocessor 204 or displayed on the display 328. In another embodiment thedevice 400 is an image projector that receives data from the electronicdata processing system 210. In addition, temperature sensors located ineither the AACMM 100 or the device 400 may be shared by the other. Itshould be appreciated that embodiments of the present invention provideadvantages in providing a flexible interface that allows a wide varietyof accessory devices 400 to be quickly, easily and reliably coupled tothe AACMM 100. Further, the capability of sharing functions between theAACMM 100 and the device 400 may allow a reduction in size, powerconsumption and complexity of the AACMM 100 by eliminating duplicity.

In one embodiment, the controller 408 may alter the operation orfunctionality of the probe end 401 of the AACMM 100. For example, thecontroller 408 may alter indicator lights on the probe housing 102 toeither emit a different color light, a different intensity of light, orturn on/off at different times when the device 400 is attached versuswhen the probe housing 102 is used by itself. In one embodiment, thedevice 400 includes a range finding sensor (not shown) that measures thedistance to an object. In this embodiment, the controller 408 may changeindicator lights on the probe housing 102 in order to provide anindication to the operator how far away the object is from the probe tip118. In another embodiment, the controller 408 may change the color ofthe indicator lights based on the quality of the image acquired by thecoded structured light scanner device. This provides advantages insimplifying the requirements of controller 420 and allows for upgradedor increased functionality through the addition of accessory devices.

Referring to FIGS. 10-13, embodiments of the present invention provideadvantages to projector, camera, signal processing, control andindicator interfaces for a non-contact three-dimensional measurementdevice 500. The device 500 includes a pair of optical devices, such as alight projector 508 and a camera 510, for example, that project astructured light pattern and receive a two-dimensional pattern that wasreflected from an object 501. The device 500 uses triangulation-basedmethods based on the known emitted pattern and the acquired image todetermine a point cloud representing the X, Y, Z coordinate data for theobject 501 for each pixel of the received image. In an embodiment, thestructured light pattern is coded so that a single image is sufficientto determine the three-dimensional coordinates of object points. Such acoded structured light pattern may also be said to measurethree-dimensional coordinates in a single shot.

In the exemplary embodiment, the projector 508 uses a visible lightsource that illuminates a pattern generator. The visible light sourcemay be a laser, a superluminescent diode, an incandescent light, a lightemitting diode (LED), or other light emitting device. In the exemplaryembodiment, the pattern generator is a chrome-on-glass slide having astructured light pattern etched thereon. The slide may have a singlepattern or multiple patterns that move in and out of position as needed.The slide may be manually or automatically installed in the operatingposition. In other embodiments, the source pattern may be lightreflected off or transmitted by a digital micro-mirror device (DMD) suchas a digital light projector (DLP) manufactured by Texas InstrumentsCorporation, a liquid crystal device (LCD), a liquid crystal on silicon(LCOS) device, or a similar device used in transmission mode rather thanreflection mode. The projector 508 may further include a lens system 515that alters the outgoing light to have the desired focalcharacteristics.

The device 500 further includes an enclosure 502 with a handle portion504. In one embodiment, the device 500 may further include an interface426 on one end that mechanically and electrically couples the device 500to the probe housing 102 as described herein above. In otherembodiments, the device 500 may be integrated into the probe housing102. The interface 426 provides advantages in allowing the device 500 tobe coupled and removed from the AACMM 100 quickly and easily withoutrequiring additional tools.

The camera 510 includes a photosensitive sensor which generates adigital image/representation of the area within the sensor's field ofview. The sensor may be charged-coupled device (CCD) type sensor or acomplementary metal-oxide-semiconductor (CMOS) type sensor for examplehaving an array of pixels. The camera 510 may further include othercomponents, such as but not limited to lens 503 and other opticaldevices for example. In the exemplary embodiment, the projector 508 andthe camera 510 are arranged at an angle such that the sensor may receivelight reflected from the surface of the object 501. In one embodiment,the projector 508 and camera 510 are positioned such that the device 500may be operated with the probe tip 118 in place. Further, it should beappreciated that the device 500 is substantially fixed relative to theprobe tip 118 and forces on the handle portion 504 may not influence thealignment of the device 500 relative to the probe tip 118. In oneembodiment, the device 500 may have an additional actuator (not shown)that allows the operator to switch between acquiring data from thedevice 500 and the probe tip 118.

The projector 508 and camera 510 are electrically coupled to acontroller 512 disposed within the enclosure 502. The controller 512 mayinclude one or more microprocessors, digital signal processors, memoryand signal conditioning circuits. Due to the digital signal processingand large data volume generated by the device 500, the controller 512may be arranged within the handle portion 504. The controller 512 iselectrically coupled to the arm buses 218 via electrical connector 434.The device 500 may further include actuators 514, 516 which may bemanually activated by the operator to initiate operation and datacapture by the device 500. In one embodiment, the image processing todetermine the X, Y, Z coordinate data of the point cloud representingobject 501 is performed by the controller 512 and the coordinate data istransmitted to the electronic data processing system 210 via bus 240. Inanother embodiment images are transmitted to the electronic dataprocessing system 210 and the calculation of the coordinates isperformed by the electronic data processing system 210.

In one embodiment, the controller 512 is configured to communicate withthe electronic data processing system 210 to receive structured lightpattern images from the electronic data processing system 210. In stillanother embodiment, the pattern emitted onto the object may be changedby the electronic data processing system 210 either automatically or inresponse to an input from the operator. This may provide advantages inobtaining higher accuracy measurements with less processing time byallowing the use of patterns that are simpler to decode when theconditions warrant, and use the more complex patterns where it isdesired to achieve the desired level of accuracy or resolution.

In other embodiments of the present invention, the device 520 (FIG. 12)includes a pair of cameras 510. The cameras 510 are arranged on an anglerelative to the projector 508 to receive reflected light from the object501. The use of multiple cameras 510 may provide advantages in someapplications by providing redundant images to increase the accuracy ofthe measurement. In still other embodiments, the redundant images mayallow for sequential patterns to be quickly acquired by the device 500by increasing the acquisition speed of images by alternately operatingthe cameras 510.

Referring now to FIG. 13A and FIG. 13B, the operation of the structuredlight device 500 will be described. The device 500 first emits astructured light pattern 522 with projector 508 onto surface 524 of theobject 501. The structured light pattern 522 may include the patternsdisclosed in the journal article “DLP-Based Structured Light 3D ImagingTechnologies and Applications” by Jason Geng published in theProceedings of SPIE, Vol. 7932, which is incorporated herein byreference. The structured light pattern 522 may further include, but isnot limited to one of the patterns shown in FIGS. 14-32. The light 509from projector 508 is reflected from the surface 524 and the reflectedlight 511 is received by the camera 510. It should be appreciated thatvariations in the surface 524, such as protrusion 526 for example,create distortions in the structured pattern when the image of thepattern is captured by the camera 510. Since the pattern is formed bystructured light, it is possible in some instances for the controller512 or the electronic data processing system 210 to determine a one toone correspondence between the pixels in the emitted pattern, such aspixel 513 for example, and the pixels in the imaged pattern, such aspixel 515 for example. This enables triangulation principals to be usedto determine the coordinates of each pixel in the imaged pattern. Thecollection of three-dimensional coordinates of the surface 524 issometimes referred to as a point cloud. By moving the device 500 overthe surface 524, a point cloud may be created of the entire object 501.It should be appreciated that in some embodiments the coupling of thedevice 500 to the probe end provides advantages in that the position andorientation of the device 500 is known by the electronic data processingsystem 210, so that the location of the object 501 relative to the AACMM100 may also be ascertained.

To determine the coordinates of the pixel, the angle of each projectedray of light 509 intersecting the object 522 in a point 527 is known tocorrespond to a projection angle phi (Φ), so that Φ information isencoded into the emitted pattern. In an embodiment, the system isconfigured to enable the Φ value corresponding to each pixel in theimaged pattern to be ascertained. Further, an angle omega (Ω) for eachpixel in the camera is known, as is the baseline distance “D” betweenthe projector 508 and the camera. Therefore, the distance “Z” from thecamera 510 to the location that the pixel has imaged using the equation:

$\begin{matrix}{\frac{Z}{D} = \frac{\sin(\Phi)}{\sin( {\Omega + \Phi} )}} & (1)\end{matrix}$Thus three-dimensional coordinates may be calculated for each pixel inthe acquired image.

In general, there are two categories of structured light, namely codedand uncoded structured light. A common form of uncoded structured light,such as that shown in FIGS. 14-17 and 28-30, relies on a striped patternvarying in a periodic manner along one dimension. These types ofpatterns are usually applied in a sequence to provide an approximatedistance to the object. Some uncoded pattern embodiments, such as thesinusoidal patterns for example, may provide relatively highly accuratemeasurements. However, for these types of patterns to be effective, itis usually necessary for the scanner device and the object to be heldstationary relative to each other. Where the scanner device or theobject are in motion (relative to the other), then a coded pattern, suchas that shown in FIGS. 18-27 may be preferable. A coded pattern allowsthe image to be analyzed using a single acquired image. Some codedpatterns may be placed in a particular orientation on the projectorpattern (for example, perpendicular to epipolar lines on the projectorplane), thereby simplifying analysis of the three-dimensional surfacecoordinates based on a single image.

Epipolar lines are mathematical lines formed by the intersection ofepipolar planes and the source plane 517 or the image plane 521 (theplane of the camera sensor) in FIG. 13B. An epipolar plane may be anyplane that passes through the projector perspective center 519 and thecamera perspective center. The epipolar lines on the source plane 517and the image plane 521 may be parallel in some cases, but in generalare not parallel. An aspect of epipolar lines is that a given epipolarline on the projector plane 517 has a corresponding epipolar line on theimage plane 521. Therefore, any particular pattern known on an epipolarline in the projector plane 517 may be immediately observed andevaluated in the image plane 521. For example, if a coded pattern isplaced along an epipolar line in the projector plane 517, the spacingbetween the coded elements in the image plane 521 may be determinedusing the values read out of the pixels of the camera sensor 510. Thisinformation may be used to determine the three-dimensional coordinatesof a point 527 on the object 501. It is further possible to tilt codedpatterns at a known angle with respect to an epipolar line andefficiently extract object surface coordinates. Examples of codedpatterns are shown in FIGS. 20-29.

In embodiments having a periodic pattern, such as a sinusoidallyrepeating pattern, the sinusoidal period represents a plurality ofpattern elements. Since there is a multiplicity of periodic patterns intwo-dimensions, the pattern elements are non-collinear. In some cases, astriped pattern having stripes of varying width may represent a codedpattern.

Referring now to FIGS. 14-17, embodiments of uncoded structured lightpatterns are shown. Some of the patterns use simple on-off (or 1, 0)type pattern and are referred to as binary patterns. In some cases, thebinary pattern is one known to have a particular sequence referred to asa gray code sequence. The term gray code as used in the field ofthree-dimensional metrology based on structured light is somewhatdifferent than the term as used in the field of electrical engineering,where the term Gray code commonly means the sequential changing of asingle bit at a time. The present application follows the use of theterm gray code as is customary for the field of three-dimensionalmetrology where the gray code typically represents a sequence of binaryblack and white values. FIG. 14A shows an example of a binary patternthat includes a plurality of sequential images 530, 532, 534, eachhaving a different stripped pattern thereon. Usually, the stripesalternate between bright (illuminated) and dark (non-illuminated)striped regions. Sometimes, the terms white and black are used to meanilluminated and non-illuminated, respectively. Thus, when the images530, 532, 534 are projected sequentially onto the surface 524 as shownin FIG. 14B which shows a composite image 536. It should be noted thatthe bottom two patterns 535, 537 of FIG. 14B are not illustrated in FIG.14A for clarity. For each point on the object 501 (represented by acamera pixel in the image) the composite pattern 536 has a unique binaryvalue obtained through the sequential projection of patterns 530, 532,534, 535, 537, which correspond to a relatively small range of possibleprojection angles Φ. By using these projection angles, together with theknown pixel angle Ω for a given pixel and the known baseline distance D,Eq. (1) may be used to find the distance Z from the camera to the objectpoint. A two-dimensional angle is known for each camera pixel. Thetwo-dimensional angle corresponds generally to the one-dimensional angleOmega, which is used in the calculation of the distance Z according toEq. (1). However, a line drawn from each camera pixel through the cameraperspective center and intersecting the object in a point defines atwo-dimensional angle in space. When combined with the calculated valueZ, the two pixel angles provide three-dimensional coordinatescorresponding to a point on the object surface.

Similarly, rather than a binary pattern, a sequential series of greypatterns having stripes with varying grey-scale values may be used. Whenused in this context, the term grey-scale usually refers to an amount ofirradiance at a point on the object from white (maximum light), tovarious levels of gray (less light), to black (minimum light). This samenomenclature is used even if the light being projected has a color suchas red, and the gray-scale values correspond to levels of redillumination. In an embodiment, the pattern (FIG. 15) has a plurality ofimages 538, 540, 542 with stripes having varying light power levels,such as black, grey and white for example, used to produce an emittedpattern on the object 501. The grey scale values may be used todetermine the possible projection angles Φ to within a relatively smallrange of possible values. As discussed hereinabove, Eq. (1) may then beused to determine the distance Z.

In another embodiment, the distance Z to an object point may be found bymeasuring a phase shift observed in a plurality of images. For example,in an embodiment shown in FIG. 16, the gray-scale intensities 546, 548,550 of a projector pattern 552 vary in a sinusoidal manner, but with thephase shifted between projected patterns. For example, in the firstprojector pattern, the sinusoid gray-scale intensity 546 (representingoptical power per unit area) may have a phase of zero degrees at aparticular point. In the second projector pattern, the sinusoidintensity 548 has a phase of 120 degrees at the same point. In the thirdprojector pattern, the sinusoid intensity 550 may have a phase of 240degrees at the same point. This is the same thing as saying that thesinusoidal pattern is shifted to the left (or right) by one-third of aperiod in each step. A phase shift method is used to determine a phaseof the projected light at each camera pixel, which eliminates the needto consider information from adjacent pixels as in the coded-patternsingle shot case. Many methods may be used to determine the phase of acamera pixel. One method involves performing a multiply and accumulateprocedure and then taking an arctangent of a quotient. This method iswell known to those of ordinary skill in the art and is not discussedfurther. In addition, with the phase shift method, the background lightcancels out in the calculation of phase. For these reasons, the value Zcalculated for a give pixel is usually more accurate than the value Zcalculated using a coded-pattern single shot method. However, with asingle collection of sinusoidal patterns such as those shown in FIG. 16,all of the calculated phases vary from 0 to 360 degrees. For aparticular structured-light triangulation system, these calculatedphases may be adequate if “thickness” of the object under test does notvary by too much because the angle for each projected stripe is knownahead of time. However, if the object is too thick, an ambiguity mayarise between in the phase calculated for a particular pixel since thatpixel may have been obtained from first projected ray of light strikingthe object at a first position or a second projected ray of lightstriking the object at a second position. In other words, if there is apossibility that the phase may vary by more than 2π radians for anypixel in the camera array, then the phases may not be properly decodedand the desired one to one correspondence not achieved.

FIG. 17A shows a sequence 1-4 of projected gray-code intensities 554according to a method by which the ambiguity may be eliminated in thedistance Z based on a calculated phase. A collection of gray codepatterns are projected sequentially onto the object. In the exampleshown, there are four sequential patterns indicated by 1, 2, 3, 4 to theleft side of 554 in FIG. 17A. The sequential pattern 1 has dark (black)on the left half of the pattern (elements 0-15) and bright (white) onthe right half of the pattern (elements 16-31). The sequential pattern 2has a dark band toward the center (elements 8-23) and bright bandstoward the edges (elements 2-7, 24-31). The sequential pattern 3 has twoseparated bright bands near the center (elements 4-11, 20-27) and threebright bands (elements 0-3, 12-19, 28-31). The sequential pattern 4 hasfour separated dark bands (elements 2-5, 10-13, 18-21, 26-29) and fiveseparated bright bands (elements 0-1, 6-9, 14-17, 22-25, 30-31). For anygiven pixel in the camera, this sequence of patterns enables the “objectthickness region” of the object to be improved by a factor of 16compared to an initial object thickness region corresponding to all theelements 0 to 31.

In another method 556 illustrated in FIG. 17C, a phase shift method,similar to the method of FIG. 16, is performed. In the embodiment shownin FIG. 17C, a pattern 556A four sinusoidal periods are projected ontoan object. For reasons discussed hereinabove, there may be an ambiguityin a distance Z to an object using the pattern of FIG. 17C. One way toreduce or eliminate the ambiguity is to project one or more additionalsinusoidal patterns 556B, 556C, each pattern having a different fringeperiod (pitch). So, for example, in FIG. 17B, a second sinusoidalpattern 555 having three fringe periods rather than four fringe periodsis projected onto an object. In an embodiment, the difference in thephases for the two patterns 555, 556 may be used to help eliminate anambiguity in the distance Z to the target.

Another method for eliminating ambiguity is to use a different type ofmethod, such as the gray code method of FIG. 17A for example, toeliminate the ambiguity in the distances Z calculated using thesinusoidal phase shift method.

In applications where the object and device 500 are in relative motion,it may be desirable to use a single pattern that allows the camera 510to capture an image that provides sufficient information to measure thethree dimensional characteristics of the object 501 without having toproject sequential images. Referring now to FIG. 18 and FIG. 19,patterns 558, 566 have a distribution of colors that may in some casesenable measurement of the object to be based on a single (coded) image.In the embodiment of FIG. 18, the pattern 558 uses lines having acontinuously spatially varying wavelength of light to create a patternwhere the color changes continuously from blue to green to yellow to redto fuchsia for example. Thus for each particular spectral wavelength, aone-to-one correspondence may be made between the emitted image and theimaged pattern. With the correspondence established, thethree-dimensional coordinates of the object 501 may be determined from asingle imaged pattern. In one embodiment, the stripes of the pattern 558are oriented perpendicular to the epipolar lines on the projector plane.Since the epipolar lines on the projector plane map into epipolar lineson the camera image plane, it is possible to obtain an associationbetween projector points and camera points by moving along the directionof epipolar lines in the camera image plane and noting the color of theline in each case. It should be appreciated that each pixel in thecamera image plane corresponds to a two-dimensional angle. The colorenables determination of the one-to-one correspondence betweenparticular projection angles and particular camera angles. Thiscorrespondence information, combined with the distance between thecamera and the projector (the baseline distance D) and the angles of thecamera and projector relative to the baseline, is sufficient to enabledetermination of the distance Z from the camera to the object.

Another embodiment using color patterns is shown in FIG. 19. In thisembodiment, a plurality of colored patterns having varying intensities560, 562, 564 are combined to create a color pattern 566. In oneembodiment, the plurality of colored patterns intensities 560, 562, 564are primary colors, such that pattern 560 varies the intensity of thecolor red, pattern 562 varies the intensity of the color green andpattern 564 varies the intensity of the color blue. Since the ratios ofcolors are known, the resulting emitted image has a known relationshipthat may be decoded in the imaged pattern. As with the embodiment ofFIG. 18, once the correspondence established, the three-dimensionalcoordinates of the object 501 may be determined. Unlike the pattern ofFIG. 18, in which a single cycle of unique colors are projected, thepattern of FIG. 19 projects three complete cycles of nearly identicalcolors. With the pattern of FIG. 18, there is little possibility ofambiguity in the measured distance Z (at least for the case in which theprojected lines are perpendicular to epipolar lines) since each camerapixel recognizes a particular color that corresponds uniquely to aparticular projection direction. Since the camera angle and projectionangles are known, triangulation may be used to determine thethree-dimensional object coordinates at each pixel position using only asingle camera image. Hence the method of FIG. 18 may be considered to bea coded, single-shot method. In contrast, in FIG. 19, there is a chanceof ambiguity in the distance Z to an object point. For example, if thecamera sees a color purple, the projector may have projected any ofthree different angles. Based on the triangulation geometry, threedifferent distances Z are possible. If the thickness of the object isknown ahead of time to be within a relatively small range of values,then it may be possible to eliminate two of the values, therebyobtaining three-dimensional coordinates in a single shot. In the generalcase, however, it would be necessary to use additional projectedpatterns to eliminate the ambiguity. For example, the spatial period ofthe colored pattern may be changed, and then used to illuminate theobject a second time. In this instance, this method of projectedstructured light is considered to be a sequential method rather than acoded, single-shot method.

Referring now to FIGS. 20-23, coded structured light patterns for asingle image acquisition are shown based on a stripe indexing technique.In the embodiments of FIG. 20 and FIG. 21, patterns having color stripes568, 570 are emitted by the projector 508. This technique utilizes acharacteristic of image sensors wherein the sensor has three independentcolor channels, such as red, green, blue or cyan, yellow, magenta forexample. The combinations of the values generated by these sensorchannels may produce a large number of colored patterns. As with theembodiment of FIG. 19, the ratio of the color distribution is known,therefore the relationship between the emitted pattern and the imagedpattern may be determined and the three-dimensional coordinatescalculated. Still other types of colored patterns may be used, such as apattern based on the De Bruijn sequence. The stripe indexing techniquesand the De Bruijn sequence are well known to those of ordinary skill inthe art and so are not discussed further.

In the embodiments of FIG. 22 and FIG. 23, a non-color stripe indexingtechnique is used. In the embodiment of FIG. 22, the pattern 572provides groups of stripes having multiple intensity (gray-scale) levelsand different widths. As a result, a particular group of stripes withinthe overall image has a unique gray-scale pattern. Due to the uniquenessof the groups, a one-to-one correspondence may be determined between theemitted pattern and the imaged pattern to calculate the coordinates ofthe object 501. In the embodiment of FIG. 23, the pattern 574 provides aseries of stripes having a segmented pattern. Since each line has uniquesegment design, the correspondence may be determined between the emittedpattern and the imaged pattern to calculate the coordinates of theobject 501. In FIGS. 20-23, additional advantages may be gained byorienting the projected lines 572, 574 perpendicular to epipolar linesso that in the camera plane since this simplifies determination of asecond dimension in finding the one-to-one correspondence between cameraand projector patterns.

Referring now to FIGS. 24-27, coded structured light patterns are shownthat use a two-dimensional spatial grid pattern technique. These typesof patterns are arranged such that a sub window, such as window 576 onpattern 578 for example, is unique relative to other sub windows withinthe pattern. In the embodiment of FIG. 24, a pseudo random binary arraypattern 578 is used. The pattern 578 uses a grid with elements, such ascircles 579 for example, that form the coded pattern. It should beappreciated that elements having other geometric shapes may also beused, such as but not limited to squares, rectangles, and triangles forexample. In the embodiment of FIG. 25, a pattern 580 is shown of amulti-valued pseudo random array wherein each of the numerical valueshas an assigned shape 582. These shapes 582 form a unique sub-window 584that allows for correspondence between the emitted pattern and theimaged pattern to calculate the coordinates of the object 501. In theembodiment of FIG. 26, the grid 586 is color coded with stripesperpendicular to the projector plane. The pattern of FIG. 26 will notnecessarily provide a pattern that can be decoded in a single shot, butthe color information may help to simplify the analysis. In theembodiment of FIG. 27, an array 588 of colored shapes, such as squaresor circles, for example, are used to form the pattern.

Referring now to FIGS. 28A-28B, an exemplary sinusoidal pattern 720 isshown. In an embodiment, the lines 734 are perpendicular to epipolarlines on the projector plane. The sinusoidal pattern 720 is made up ofthirty lines 722 which are repeated once to give a total number of lines722 of sixty. Each line 722 has a sinusoidal feature 723 that isapproximately 180 degrees out of phase with the line above and the linebelow. This is to allow the lines 722 to be as close as possible andalso allows a greater depth of field because the lines can blur on theprojected surface or acquired image and still be recognized. Each singleline 722 can be uniquely decoded using just the phase of that line wherethe line length must be at least one wavelength of the sinusoid.

Since the pattern 720 is repeated, it would generally cause ambiguitiesin the line identification. However this is problem is resolved in thissystem through the geometry of the camera's field of view and depth offield. For a single view of the camera, i.e. a row of pixels, within thedepth of field in which the lines can be optically resolved, no twolines with the same phase can be imaged. For example, the first row ofpixels on the camera can only receive reflected light from lines 1-30 ofthe pattern. Whereas further down the camera sensor, another row willonly receive reflected light from lines 2-31 of the pattern, and so on.In FIG. 28B an enlarged portion of the pattern 720 is shown of threelines where the phase between consecutive lines 722 is approximately 180degrees. It also shows how the phase of each single line is enough touniquely decode the lines.

Referring now to FIGS. 29A-29B, another pattern 730 is shown havingsquare pattern elements. In an embodiment, the lines 732 areperpendicular to epipolar lines on the projector plane. The squarepattern 730 contains twenty seven lines 732 before the pattern 730 isrepeated and has a total number of lines of 59. The code elements 734 ofpattern 730 are distinguished by the phase of the square wave from leftto right in FIG. 29B. The pattern 730 is encoded such that a group ofsequential lines 732 are distinguished by the relative phases of itsmembers. Within the image, sequential lines are found by scanningvertically for the lines. In an embodiment, scanning vertically meansscanning along epipolar lines in the camera image plane. Sequentiallines within a camera vertical pixel column are paired together andtheir relative phases are determined. Four sequential paired lines arerequired to decode the group of lines and locate them within the pattern730. There is also an ambiguity in this pattern 730 due to the repeatbut this is also solved in the same manner as discussed above withrespect to sinusoidal pattern 720. FIG. 29B shows an enlarged view offour lines 732 of the square pattern. This embodiment shows that thephase of a single line 732 alone is not able to uniquely decode a linebecause the first and third lines have the same absolute phase.

This approach to code the relative phases versus the absolute phasesprovides advantages in that there is a higher tolerance for thepositions of the phases. Minor errors in the construction of theprojector which may cause the phases of the lines to shift throughoutthe depth of field of the camera, as well as errors due to the projectorand camera lenses make an absolute phase much more difficult todetermine. This can be overcome in the absolute phase method byincreasing the period such that it is sufficiently large enough toovercome the error in determining the phase.

It should be appreciated that for the case of a two-dimensional patternthat projects a coded pattern of light, the three non-collinear patternelements are recognizable because of their codes, and since they areprojected in two dimensions, the at least three pattern elements arenon-collinear. For the case of the periodic pattern, such as thesinusoidally repeating pattern, each sinusoidal period represents aplurality of pattern elements. Since there is a multiplicity of periodicpatterns in two dimensions, the pattern elements are non-collinear. Incontrast, for the case of the laser line scanner that emits a line oflight, all of the pattern elements lie on a straight line. Although theline has width and the tail of the line cross section may have lessoptical power than the peak of the signal, these aspects of the line arenot evaluated separately in finding surface coordinates of an object andtherefore do not represent separate pattern elements. Although the linemay contain multiple pattern elements, these pattern elements arecollinear.

Further, the various pattern techniques may be combined as shown inFIGS. 30-31 to form either a binary (FIG. 30) checkerboard uncodedpattern 590 or a colored (FIG. 31) checkerboard uncoded pattern 592. Instill another embodiment shown in FIG. 32, a photometric stereotechnique may be used where a plurality of images 594 are taken on theobject 501 where the light source 596 is moved to a plurality oflocations.

Referring now to FIG. 33, another embodiment is shown of a system 700for acquiring three-dimensional coordinates of an object 702. In thisembodiment, the device 704 is independently operable when detached fromthe AACMM 100. The device 704 includes a controller 706 and an optionaldisplay 708. The display 708 may be integrated in the housing of thedevice 704 or may be a separate component that is coupled to the device704 when it is used independently from the AACMM 100. In embodimentswhere the display 708 is separable from the device 704, the display 708may include a controller (not shown) that provides additionalfunctionality to facilitate to independent operation of the device 704.In one embodiment, the controller 706 is disposed within the separabledisplay.

The controller 706 includes a communications circuit configured towirelessly transmit data, such as images or coordinate data via acommunications link 712 to the AACMM 100, to a separate computing device710 or a combination of both. The computing device 710 may be, but isnot limited to a computer, a laptop, a tablet computer, a personaldigital assistant (PDA), or a cell phone for example. The display 708may allow the operator see the acquired images, or the point cloud ofacquired coordinates of the object 702. In one embodiment, thecontroller 706 decodes the patterns in the acquired image to determinethe three-dimensional coordinates of the object. In another embodiment,the images are acquired by the device 704 and transmitted to either theAACMM 100, the computing device 710 or a combination of both.

The device 704 may further include a location device assembly 714. Thelocation device assembly may include one or more of inertial navigationsensors, such as a Global Positioning System (GPS) sensor, a gyroscopicsensor, an accelerometer sensor. Such sensors may be electricallycoupled to the controller 706. Gyroscopic and accelerometer sensors maybe single-axis or multiple-axis devices. The location device assembly714 is configured to allow the controller 706 to measure or maintain theorientation of the device 704 when detached from the AACMM 100. Agyroscope within the location device assembly 714 may be a MEMSgyroscopic device, a solid-state ring-laser device, a fiber optic devicegyroscope, or other type.

When the device 704 is removed from the articulated arm CMM 100, amethod is used to combine images obtained from multiple scans. In anembodiment the images are each obtained by using coded patterns so thatonly a single image is needed to obtain three-dimensional coordinatesassociated with a particular position and orientation of the device 704.One way to combine multiple images captured by the device 704 is toprovide at least some overlap between adjacent images so that pointcloud features may be matched. This matching function may be assisted bythe inertial navigation devices described above.

Another method that can be used to assist in accurate registration ofimages collected by the device 704 is the use of reference markers. Inan embodiment, the reference markers are small markers having anadhesive or sticky backing, for example, circular markers that areplaced on an object or objects being measured. Even a relatively smallnumber of such markers can be useful in registering multiple images,especially if the object being measured has a relatively small number offeatures to use for registration. In an embodiment, the referencemarkers may be projected as spots of light onto the object or objectsunder inspection. For example, a small portable projector capable ofemitting a plurality of small dots may be placed in front of the objector objects to be measured. An advantage of projected dots over stickydots is that the dots do not have to be attached and later removed.

In one embodiment, the device projects the structured light over acontiguous and enclosed area 716 and can acquire an image over the area716 at a range of 100 mm to 300 mm with an accuracy of 35 microns. In anembodiment, the perpendicular area 716 of projection is approximately150 to 200 mm². The camera or cameras 510 may be a digital camera havinga 1.2-5.0 megapixel CMOS or CCD sensor.

Referring to FIG. 28 and FIG. 29, the process of decoding a codedpattern will be described. The first step in decoding an image of thepattern is to extract the centers of gravity (cog) 724 (FIG. 28C) of theprojected pattern 720 features in the Y direction. This is carried outby calculating a moving average of the pixel grayscale values and movingdownwards in the Y direction processing a single column at a time. Whena pixel value in an image falls above the moving average value then astarting point for a feature is found. After a starting point is foundthe width of the feature continues to increase until a pixel value fallsbelow the moving average value. A weighted average is then calculatedusing the pixel values and their Y positions between the start and endpoints to give the cog 724 of the pattern feature 723 in the image. Thedistances between the start and end points are also recorded for lateruse.

The resulting cogs 724 are used next to find the pattern lines 722. Thisis done by moving in a left to right direction (when viewed from thedirection shown in the Figures) starting with the first column of theimage. For each cog 724 in this column the neighboring column to theimmediate right is searched for a cog 724 that is within a particulardistance. If two matching cogs 724 are found then a potential line hasbeen determined. As the process moves across the image more new linesare determined and other previously determined lines are extended inlength as additional cogs 724 are detected within the tolerance. Oncethe entire image has been processed a filter is applied to the extractedlines to ensure only lines of a desired length, which is the wavelengthof the pattern, are used in the remaining steps. FIG. 28C also shows thedetected lines where they are all longer than a single wavelength of thepattern. In one embodiment there is no or a small delta betweenneighboring column's cogs.

The next step in the decoding process is to extract the projectedpattern features along the lines in the X direction in the form of blockcenters. Each pattern contains both wide blocks and narrow blocks. Inthe sinusoidal pattern 720 this refers to the peaks and valleys of thewave and in the square pattern 730 this refers to the wide squares andthe narrow squares. This process proceeds in a similar fashion toextracting the features in the Y direction, however the moving averageis also calculated using the widths found in the first stage and thedirection of movement is along the line. As described above, thefeatures are extracted in the area where widths are above the movingaverage value but in this process, features are also extracted in theareas where the widths are below the moving average. The widths and Xpositions are used to calculate a weighted average to find the center ofthe block 726 in the X direction. The Y positions of the cogs 724between moving average crossings are also used to calculate a center forthe block 726 in the Y direction. This is carried out by taking theaverage of the Y coordinates of the cogs. The start and end points ofeach line are also modified based on the features extracted in this stepto ensure that both points are where the crossing of the moving averageoccurs. In one embodiment, only complete blocks are used in laterprocessing steps.

The lines and blocks are then processed further to ensure that thedistance between the block centers 726 on each line are within apredetermined tolerance. This is accomplished by taking the deltabetween the X center positions between two neighboring blocks on a lineand checking that the delta is below the tolerance. If the delta isabove the tolerance then the line is broken up into smaller lines. Ifthe break is required between the last two blocks on a line then thelast block is removed and no additional line is created. If the break isrequired between the first and second or second and third blocks on aline then the blocks to the left of the break are also discarded and noadditional line is created. For situations where the break occurs in anyother place along the line the line is broken into two and a new line iscreated and the appropriate blocks are transferred to it. After thisstage of processing the two patterns require different steps to finishdecoding.

The sinusoidal pattern 720 may now be decoded with one additional stepof processing using the block centers on the lines. The modulus of eachblock X center and the wavelength of the pattern 720 on a line 722 arecalculated and the average of these values gives the phase of the line722. The phase of the line 722 may then be used to decode the line inthe pattern 720 which in turn allows for the determination of an X, Y, Zcoordinate position for all cogs 724 on that line 722.

Before the square pattern 730 is decoded, first lines 732 be connectedvertically before any decoding can take place. This allows a group oflines to be identified and not just a single line like the sinusoidalpattern. Connections 736 are found between lines 732 by using the blocks734 and the cogs contained in the block calculated in the first stage ofprocessing. The first cog in each block on a line 732 is tested to seeif there is another cog directly below it in the same column. If thereis no cog below then there is no connection with another line at thispoint so processing continues. If there is a cog below then the Ydistance between the two cogs is determined and compared to a desiredmaximum spacing between lines. If the distance is less than this valuethe two lines are considered connected at that point and the connection736 is stored and processing continues onto the next block. In oneembodiment, a line connection 736 is unique such that no two lines willhave more than one connection 736 between them.

The next step of processing for the square pattern 730 is phasecalculation between connected lines. Each pair of lines 732 is firstprocessed to determine the length of overlap between them. In oneembodiment there is at least one wavelength of overlap between the pairof lines to allow the calculation of the relative phase. If the lineshave the desired overlap, then the cog at center of the area of overlapis found. The blocks 738 that contain the center cog and the cogdirectly below are determined and the relative phase between the block Xcenters is calculated for that line connection. This process is repeatedfor all connections between lines. In one embodiment, the process isrepeated in only the downwards direction in the Y axis. This is becausethe code is based on connections below lines and not the other way roundor both. FIG. 29C shows the blocks 738 that could be used forcalculating the relative phase for this set of lines. The relativephases in embodiment of FIG. 29C are 3, 1 and 2 and these phases wouldbe used in the final stage to decode the top line.

The next step in decoding the square pattern 730 is performing a look upusing the relative phases calculated in the previous step. Each line 732is processed by tracking down the line connections 736 until aconnection depth of four is reached. This depth is used because this isthe number of phases to decode the line. At each level of the connectiona hash is determined using the relative phase between the lines 732.When the required connection depth is reached the hash is used to lookup the line code. If the hash returns a valid code then this is recordedand stored in a voting system. Every line 732 is processed in this wayand all connections that are of the desired depth are used to generate avote if they are a valid phase combination. The final step is then tofind out which code received the most votes on each line 732 andassigned the code of the line 732 to this value. If there is not aunique code that received the most votes then the line is not assigned acode. The lines 732 are identified once a code has been assigned and theX, Y, Z coordinate position for all cogs on that line 732 may now befound.

It should be noted that although the descriptions given abovedistinguish between line scanners and area (structured light) scannersbased on whether three or more pattern elements are collinear, it shouldbe noted that the intent of this criterion is to distinguish patternsprojected as areas and as lines. Consequently patterns projected in alinear fashion having information only along a single path are stillline patterns even though the one-dimensional pattern may be curved.

While the invention has been described with reference to exampleembodiments, it will be understood by those skilled in the art thatvarious changes may be made and equivalents may be substituted forelements thereof without departing from the scope of the invention. Inaddition, many modifications may be made to adapt a particular situationor material to the teachings of the invention without departing from theessential scope thereof. Therefore, it is intended that the inventionnot be limited to the particular embodiment disclosed as the best modecontemplated for carrying out this invention, but that the inventionwill include all embodiments falling within the scope of the appendedclaims. Moreover, the use of the terms first, second, etc. do not denoteany order or importance, but rather the terms first, second, etc. areused to distinguish one element from another. Furthermore, the use ofthe terms a, an, etc. do not denote a limitation of quantity, but ratherdenote the presence of at least one of the referenced item.

What is claimed is:
 1. A portable articulated arm coordinate measuringmachine (AACMM) for measuring three-dimensional coordinates of an objectin space, comprising: a base; a manually positionable arm portion havingan opposed first end and second end, the arm portion being rotationallycoupled to the base, the arm portion including a plurality of connectedarm segments, each arm segment including at least one positiontransducer for producing a position signal; an electronic circuit whichreceives the position signal from the at least one position transducerin each arm segment; a probe end coupled to the first end; a noncontactthree-dimensional measuring device coupled to the probe end, thenoncontact three-dimensional measuring device having a projector and animage sensor, the projector having a source plane, the projectorconfigured to emit a structured light onto the object, the structuredlight emitted from the source plane and including at least threenon-collinear pattern elements, the image sensor arranged to receive thestructured light reflected from the object; and a processor electricallycoupled to the electronic circuit, the processor configured to determinethe three-dimensional coordinates of a point on the object in responseto receiving the position signals from the position transducers and inresponse to receiving the structured light by the image sensor.
 2. TheAACMM of claim 1 wherein the noncontact three-dimensional measuringdevice is removably coupled to the probe end.
 3. The AACMM of claim 1wherein the structured light is a coded structured light pattern.
 4. TheAACMM of claim 3 wherein the noncontact three-dimensional measuringdevice is independently operable when detached from the probe end. 5.The AACMM of claim 3 wherein the coded structured light patterncomprises graphical elements that include at least one of a square,rectangle and triangle.
 6. The AACMM of claim 5 wherein the coded lightpattern is a sinusoidal pattern that includes 30 lines and each line is180 degrees out of phase with respect to adjacent lines.
 7. The AACMM ofclaim 5 wherein the coded structured light pattern includes 27 lines andthe graphical elements are squares.
 8. The AACMM of claim 3 wherein thecoded structured light includes a pattern having a plurality ofwavelengths, wherein at least one wavelength has a different spatialarrangement than the other wavelengths.
 9. The AACMM of claim 3 whereinthe coded structured light includes a pattern having a plurality ofdistinct colors.
 10. The AACMM of claim 3 wherein the coded structuredlight includes a segmented line pattern.
 11. The AACMM of claim 3wherein the coded structured light includes a two-dimensional spatialgrid pattern.
 12. The AACMM of claim 11 wherein the two-dimensionalspatial grid pattern includes a pseudo-random binary array.
 13. TheAACMM of claim 11 wherein the two-dimensional spatial grid patternincludes a color coded grid.
 14. The AACMM of claim 11 wherein thetwo-dimensional spatial grid pattern includes a multi-valued pseudorandom array.
 15. The AACMM of claim 11 wherein the two-dimensionalspatial grid pattern includes a two-dimensional array of color-codedgeometric shapes.
 16. The AACMM of claim 1 wherein the structured lightpattern is an uncoded structured light pattern.
 17. The AACMM of claim16 wherein the uncoded structured light pattern includes sequentialprojection images.
 18. The AACMM of claim 17 wherein the sequentialprojection images are a set of binary patterns.
 19. The AACMM of claim17 wherein the sequential projection images are a set of patternsincluding stripes having at least two levels of intensity.
 20. The AACMMof claim 17 wherein the sequential projection images are a set of atleast three sinusoidal patterns.
 21. The AACMM of claim 17 wherein thesequential projection images are a set of patterns including stripeshaving at least two levels of intensity which include at least threesinusoidal patterns.
 22. The AACMM of claim 16 wherein the uncodedstructured light pattern projects a sequence of different illuminatedpatterns, each of the sequence of different illuminated patterns beingprojected from different locations relative to the object.
 23. The AACMMof claim 16 wherein the uncoded structured light pattern includes arepeated grey scale pattern.
 24. The AACMM of claim 1 further comprisinga contact measurement device coupled to the probe end.
 25. The AACMM ofclaim 1 wherein the processor is located within the noncontactthree-dimensional measuring device.
 26. A method of operating a portablearticulated arm coordinate measuring machine for measuring thecoordinates of an object in space, comprising: providing a manuallypositionable arm portion having an opposed first end and second end, thearm portion including a plurality of connected arm segments, each armsegment including at least one position transducer for producing aposition signal; providing a probe end for measuring the object, theprobe end being coupled to the first end; receiving at an electroniccircuit the position signals from the transducers; providing athree-dimensional noncontact measurement device having a controller, thethree-dimensional noncontact measurement device having a sensor and aprojector, the projector configured to emit a structured light onto theobject, the projector having a source plane, the structured lightemitted from the source plane and including at least three non-collinearpattern elements; and projecting a structured light from thethree-dimensional measurement device onto the object.
 27. The method ofclaim 26 further comprising receiving a reflection of the structuredlight from the object with the three-dimensional measurement device. 28.The method of claim 27 further comprising determining three-dimensionalcoordinates of a point on the object from the reflected structuredlight.
 29. The method of claim 28 wherein the structured light is acoded structured light.
 30. The method of claim 29 wherein the codedstructured light pattern projected onto the object comprises graphicalelements that include at least one of a square, rectangle and triangle.31. The method of claim 29 wherein the coded light pattern is asinusoidal pattern that includes 30 lines and each line is 180 degreesout of phase with respect to adjacent lines.
 32. The method of claim 29wherein the coded structured light pattern includes 27 lines and thegraphical elements are squares.
 33. The method of claim 29 wherein thecoded structured light includes a pattern having a plurality ofwavelengths, wherein at least one wavelength has a different spatialarrangement than the other wavelengths.
 34. The method of claim 33wherein the pattern having a plurality of wavelengths is arranged intolines oriented substantially perpendicular to the source plane.
 35. Themethod of claim 29 wherein the coded structured light includes a singlepattern having a plurality of distinct colors.
 36. The method of claim29 wherein the coded structured light includes a segmented line pattern.37. The method of claim 29 wherein the coded structured light includes atwo-dimensional spatial grid pattern.
 38. The method of claim 37 whereinthe two-dimensional spatial grid pattern includes a pseudo-random binaryarray.
 39. The method of claim 37 wherein the two-dimensional spatialgrid pattern includes a color coded grid.
 40. The method of claim 37wherein the two-dimensional spatial grid pattern includes a multi-valuedpseudo random array.
 41. The method of claim 37 wherein thetwo-dimensional spatial grid pattern includes a two-dimensional array ofcolor-coded geometric shapes.
 42. The method of claim 29 furthercomprising changing the coded structured light from a first pattern to asecond pattern with the electronic circuit.
 43. The method of claim 42wherein the coded structured light is changed in response to an operatorinput.
 44. The method of claim 42 wherein the coded structured light ischanged automatically by the electronic circuit in response to a changein conditions on the object.
 45. The AACMM of claim 28 furthercomprising: separating the three-dimensional measurement device from theprobe end; and operating the three-dimensional measurement deviceseparately from the probe end.
 46. The AACMM of claim 45 furthercomprising transmitting data from the three-dimensional measurementdevice operating separately from the probe end.